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- IIL_IS-10 abstract "The IIL IS-10 was a high performance, single seat glider, designed and built in Romania in the early 1960s. It was the first Romanian aircraft to use laminar flow airfoils.".
- IIL_IS-10 origin Romania.
- IIL_IS-10 predecessor IIL_IS-4.
- IIL_IS-10 type Glider_(sailplane).
- IIL_IS-10 wikiPageID "41671916".
- IIL_IS-10 wikiPageRevisionID "597745076".
- IIL_IS-10 airfoil "NACA 634621 root, 632618 from mid span outwards".
- IIL_IS-10 aspectRatio "17".
- IIL_IS-10 crew "One".
- IIL_IS-10 designer "Iosif Silimon".
- IIL_IS-10 developedFrom IIL_IS-4.
- IIL_IS-10 emptyWeightKg "240".
- IIL_IS-10 firstFlight "1960-04-06".
- IIL_IS-10 glideRatio "best 32.7 at".
- IIL_IS-10 grossWeightKg "340".
- IIL_IS-10 heightM "1.6".
- IIL_IS-10 lengthM "7.44".
- IIL_IS-10 manufacturer "Intreprinderea de industrie Locală".
- IIL_IS-10 nationalOrigin Romania.
- IIL_IS-10 neverExceedSpeedKmh "230".
- IIL_IS-10 neverExceedSpeedNote "placard, in smooth air *Rough air speed max: *Aerotow speed: *Winch launch speed:".
- IIL_IS-10 primeUnits%3F_ "met".
- IIL_IS-10 ref "Sailplanes of the World, pp.202-3".
- IIL_IS-10 sinkRateMs "0.67".
- IIL_IS-10 sinkRateNote "minimum, at".
- IIL_IS-10 spanM "15".
- IIL_IS-10 stallSpeedKmh "62".
- IIL_IS-10 type "Single seat glider".
- IIL_IS-10 wingAreaSqm "13.2".
- IIL_IS-10 m "25.7".
- IIL_IS-10 subject Category:Romanian_sailplanes_1960–1969.
- IIL_IS-10 type Aircraft.
- IIL_IS-10 type MeanOfTransportation.
- IIL_IS-10 type Product.
- IIL_IS-10 type DesignedArtifact.
- IIL_IS-10 comment "The IIL IS-10 was a high performance, single seat glider, designed and built in Romania in the early 1960s. It was the first Romanian aircraft to use laminar flow airfoils.".
- IIL_IS-10 label "IIL IS-10".
- IIL_IS-10 sameAs m.0_ft1nq.
- IIL_IS-10 sameAs Q17079953.
- IIL_IS-10 sameAs Q17079953.
- IIL_IS-10 wasDerivedFrom IIL_IS-10?oldid=597745076.
- IIL_IS-10 isPrimaryTopicOf IIL_IS-10.